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WO2012001492A1 - Procédé pour commander la mise à température d'un dispositif d'extrusion destiné à produire un produit semi-fini en élastomère - Google Patents

Procédé pour commander la mise à température d'un dispositif d'extrusion destiné à produire un produit semi-fini en élastomère Download PDF

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Publication number
WO2012001492A1
WO2012001492A1 PCT/IB2011/001515 IB2011001515W WO2012001492A1 WO 2012001492 A1 WO2012001492 A1 WO 2012001492A1 IB 2011001515 W IB2011001515 W IB 2011001515W WO 2012001492 A1 WO2012001492 A1 WO 2012001492A1
Authority
WO
WIPO (PCT)
Prior art keywords
working temperature
elastomeric material
structural units
temperature
heating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/IB2011/001515
Other languages
English (en)
Inventor
Cesare Emanuele Amurri
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pirelli and C SpA
Pirelli Tyre SpA
Original Assignee
Pirelli SpA
Pirelli Tyre SpA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Pirelli SpA, Pirelli Tyre SpA filed Critical Pirelli SpA
Priority to JP2013517568A priority Critical patent/JP5802271B2/ja
Priority to EP11743336.7A priority patent/EP2585272B1/fr
Priority to CN201180030362.XA priority patent/CN102958671B/zh
Priority to KR1020127033188A priority patent/KR101860449B1/ko
Priority to BR112012031733-4A priority patent/BR112012031733B1/pt
Priority to US13/807,177 priority patent/US9403309B2/en
Publication of WO2012001492A1 publication Critical patent/WO2012001492A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/14—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the particular extruding conditions, e.g. in a modified atmosphere or by using vibration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17—Component parts, details or accessories; Auxiliary operations
    • B29C45/72—Heating or cooling
    • B29C45/74—Heating or cooling of the injection unit
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17—Component parts, details or accessories; Auxiliary operations
    • B29C45/76—Measuring, controlling or regulating
    • B29C45/78—Measuring, controlling or regulating of temperature
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/022—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the choice of material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/36—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/365—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using pumps, e.g. piston pumps
    • B29C48/37—Gear pumps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/36—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/395—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using screws surrounded by a cooperating barrel, e.g. single screw extruders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B29C48/875—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling for achieving a non-uniform temperature distribution, e.g. using barrels having both cooling and heating zones
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/92—Measuring, controlling or regulating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00—Indexing scheme relating to extrusion moulding
    • B29C2948/92—Measuring, controlling or regulating
    • B29C2948/92323—Location or phase of measurement
    • B29C2948/92485—Start-up, shut-down or parameter setting phase; Emergency shut-down; Material change; Test or laboratory equipment or studies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00—Indexing scheme relating to extrusion moulding
    • B29C2948/92—Measuring, controlling or regulating
    • B29C2948/92504—Controlled parameter
    • B29C2948/92704—Temperature
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00—Indexing scheme relating to extrusion moulding
    • B29C2948/92—Measuring, controlling or regulating
    • B29C2948/92819—Location or phase of control
    • B29C2948/92857—Extrusion unit
    • B29C2948/92876—Feeding, melting, plasticising or pumping zones, e.g. the melt itself
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00—Indexing scheme relating to extrusion moulding
    • B29C2948/92—Measuring, controlling or regulating
    • B29C2948/92819—Location or phase of control
    • B29C2948/92857—Extrusion unit
    • B29C2948/92876—Feeding, melting, plasticising or pumping zones, e.g. the melt itself
    • B29C2948/92895—Barrel or housing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00—Indexing scheme relating to extrusion moulding
    • B29C2948/92—Measuring, controlling or regulating
    • B29C2948/92819—Location or phase of control
    • B29C2948/92857—Extrusion unit
    • B29C2948/92904—Die; Nozzle zone
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00—Indexing scheme relating to extrusion moulding
    • B29C2948/92—Measuring, controlling or regulating
    • B29C2948/92819—Location or phase of control
    • B29C2948/9298—Start-up, shut-down or parameter setting phase; Emergency shut-down; Material change; Test or laboratory equipment or studies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/07—Flat, e.g. panels
    • B29C48/08—Flat, e.g. panels flexible, e.g. films
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/09—Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/269—Extrusion in non-steady condition, e.g. start-up or shut-down
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/36—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/375—Plasticisers, homogenisers or feeders comprising two or more stages
    • B29C48/387—Plasticisers, homogenisers or feeders comprising two or more stages using a screw extruder and a gear pump
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B29C48/80—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling at the plasticising zone, e.g. by heating cylinders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B29C48/80—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling at the plasticising zone, e.g. by heating cylinders
    • B29C48/83—Heating or cooling the cylinders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B29C48/80—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling at the plasticising zone, e.g. by heating cylinders
    • B29C48/83—Heating or cooling the cylinders
    • B29C48/832—Heating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B29C48/80—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling at the plasticising zone, e.g. by heating cylinders
    • B29C48/84—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling at the plasticising zone, e.g. by heating cylinders by heating or cooling the feeding screws
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/78—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling
    • B29C48/86—Thermal treatment of the extrusion moulding material or of preformed parts or layers, e.g. by heating or cooling at the nozzle zone
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D30/00—Producing pneumatic or solid tyres or parts thereof
    • B29D30/06—Pneumatic tyres or parts thereof (e.g. produced by casting, moulding, compression moulding, injection moulding, centrifugal casting)
    • B29D30/08—Building tyres
    • B29D30/10—Building tyres on round cores, i.e. the shape of the core is approximately identical with the shape of the completed tyre
    • B29D30/16—Applying the layers; Guiding or stretching the layers during application
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2021/00—Use of unspecified rubbers as moulding material
    • B29K2021/006—Thermosetting elastomers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2301/00—Use of unspecified macromolecular compounds as reinforcement
    • B29K2301/10—Thermosetting resins

Definitions

  • the present invention relates to a method for controlling the heating of an extrusion device of a semi-finished product made of elastomeric material.
  • the above-mentioned method is carried out in a process for building a component made of elastomeric material of a tyre for vehicle wheels.
  • elastomeric material is used to indicate a composition comprising at least one elastomeric polymer and at least one reinforcing filler.
  • such composition further comprises additives such as, for example, a cross-linking agent and/or a plasticizer. Thanks to the presence of the cross-linking agent, such material may be cross-linked by heating, so as to make the end product .
  • si-finished product made of elastomeric material is used to indicate an elongated element made of elastomeric material only and having a flat shape.
  • component made of elastomeric material is used to indicate any component of the tyre, or a part thereof, obtained from said semi-finished product and thus comprising elastomeric material only.
  • thermal inertia of a structural unit of an extrusion device indicates the tendency of a structural unit to withstand changes in temperature; it is higher when the mass of material constituting such structural unit is greater .
  • working temperature of a structural unit of the extrusion device indicates the temperature at which such structural unit is maintained during the extrusion process. This implies that at temperatures lower than the operating one, the extrusion process does not take place .
  • a tyre for vehicle wheels generally comprises a carcass structure comprising at least one carcass ply formed of reinforcing cords incorporated in an elastomeric matrix.
  • the carcass ply has end edges respectively engaged with annular anchoring structures.
  • the latter are arranged in the areas of the tyre usually identified by the name "beads" and they are normally formed each by a substantially circumferential annular insert on which at least one filling insert is applied, in a radially outer position thereof.
  • Such annular inserts are commonly identified as “bead cores” and have the task of keeping the tyre firmly fixed to the anchoring seat specifically provided in the rim of the wheel, thus preventing, in operation, the radially inner end edge of the tyre coming out from such a seat.
  • an airtight coating layer made of elastomeric material, typically called liner is typically provided in a radially inner position with respect to the carcass ply/plies.
  • the belt structure comprises one or more belt layers arranged radially one on top on the other and having textile or metallic reinforcement cords arranged preferably according to an inclined orientation with respect to the circumferential direction of the tyre and normally crossed with respect to the cords of the possible adjacent belt layer .
  • the belt structure can further comprise at least one reinforcing structure defined by at least one continuous reinforcing elongated element including at least one textile or metallic reinforcement cord incorporated in a matrix of elastomeric material and extending parallel to the longitudinal direction of the elongated element itself.
  • under-belt a layer of elastomeric material, called "under-belt"
  • under-belt a layer of elastomeric material, called "under-belt”
  • said layer having the function of making the radially outer surface of the carcass structure as uniform as possible for the subsequent application of the belt structure .
  • tread band In a radially outer position with respect to the belt structure a tread band is applied, also made of elastomeric material, as well as other structural elements making up the tyre.
  • Respective sidewalls of elastomeric material are also applied on the side surfaces of the carcass structure, each extending from one of the side edges of the tread band up to the respective annular anchoring structure to the beads.
  • a tyre for vehicle wheels typically comprises a plurality of components made of elastomeric material only, according to the definition given above.
  • the following components can be identified, as non-limiting examples: tread band, sidewalls, the so-called under-belt and/or under-layer layers, filling inserts of the annular anchoring structures, liner, sub-liner, sidewall inserts, reinforcing inserts, etc.
  • the above-mentioned components may be made starting from semi-finished products made of elastomeric material only, obtained by an extrusion process.
  • the extruded semifinished product is then laid on a forming support which can rotate about a rotation axis, so as to obtain a deposition preferably according to adjacent and/or at least partly superimposed coils, depending on the component to be made .
  • the extrusion process is carried out in a device consisting of a plurality of structural units having different mass, thermal inertia and working temperature, where at least some structural units having low mass and thermal inertia have a high working temperature and vice versa .
  • WO 2006/037369 in the name of the Applicant, recites that in a process for manufacturing an elastomeric tyre component, the elastomeric component is fed to an extruding device comprising a plurality of units each having a respective working temperature. Said units are heated to reach the respective working temperature, starting from the unit having the lowest working temperature up to the unit having the highest working temperature.
  • the Applicant has considered that, in order to ensure that during the extrusion process the elastomeric material fed into the extrusion device has sufficient fluidity at the required operating flow rates and pressures, all of the above units must be heated to reaching the respective working temperature prior to the feeding of the elastomeric material into the extrusion device.
  • the Applicant has further considered that in order to minimise the process times, said heating should occur as a whole in the shortest possible time.
  • the Applicant has considered that whenever the extrusion process is ended or interrupted, it is advantageous to leave some elastomeric material into the extrusion device to prevent the formation of air bubbles, which would cause troubles upon restart.
  • the Applicant has noted that a method suitable for allowing the respective working temperature to be reached by all the units making up the extrusion device as quickly as possible, without risking a vulcanization of the elastomeric material at any one of the above units and without the need of running experimental tests beforehand on the single units of the specific extrusion device used would meet even better the opposed process requirements.
  • the Applicant has understood that in order to limit the heating process cycle time as much as possible it is suitable to implement an automatic procedure that initially provides for the simultaneous heating of all the units, thus carrying out a method totally different from that described in WO 2006/037369, which instead provides for a predetermined sequence of activation of the heating starting from the unit having the lowest working temperature up to that having the highest working temperature .
  • the Applicant has further understood that in order to prevent the risk of having a vulcanization of the elastomeric material into the extrusion device, it is advisable that the above heating procedure be such as to allow the units having a low thermal inertia and a high working temperature to be the last ones reaching the respective working temperatures, that is, once the units having higher thermal mass and lower working temperature have reached their working temperatures.
  • the Applicant has perceived that such result may be effectively obtained by implementing a heating procedure that at first provides for a simultaneous heating of all the units up to a predetermined temperature value and when a predetermined unit is close to or has reached such temperature, a further simultaneous heating of the other units up to a new temperature value properly predetermined. Such further simultaneous heating is repeated several times and each time only for the units that have not yet reached the respective working temperature, such repetition continuing until all the units of the extrusion device have reached the respective working temperature.
  • the present invention therefore relates to a method for controlling the heating of an extrusion device of a semi-finished product made from elastomeric material, the extrusion device comprising a plurality of structural units, each structural unit having a working temperature different to the working temperature of at least one other structural unit and a thermal inertia different to the thermal inertia of at least one other structural unit, the method comprising:
  • the method of the present invention can advantageously be implemented on any extrusion device, preferably those with a gear pump, where mixture is always present at the end portion of the machine which may be removed only by disassembling parts of the machinery (the extruders with opening head and without gear pump usually allow the machine to be fully emptied, thus the cross-linking problem does not occur) , irrespective of the number and type of structural units that make up such extrusion device and irrespective of the difference of mass and/or thermal inertia of said structural units. In fact, in order to implement said method it is sufficient to know only the working temperature of each structural unit making up the extrusion device.
  • the present invention may have at least one
  • said iterative repetition comprises at least: e) simultaneously heating said other structural units of said extrusion device.
  • said iterative repetition also comprises at least:
  • said iterative repetition also comprises at least:
  • each structural unit has a working temperature different to the working temperature of all the other structural units.
  • each structural unit has thermal inertia different to the thermal inertia all the other structural units.
  • said plurality of structural units comprises at least one housing, at least one member for moving the elastomeric material inside said at least one housing and at least one drawing member of the elastomeric material.
  • said at least one member for moving the elastomeric material comprises an extrusion screw.
  • Such particular moving member has a relatively low working temperature and a predetermined thermal inertia.
  • said at least one housing has a working temperature higher than that of the member for moving the elastomeric material.
  • said at least one housing has a thermal inertia higher than that of the member for moving the elastomeric material .
  • said at least one drawing member comprises at least one nozzle.
  • Such particular drawing member is characterised in that it has a particularly low thermal inertia and a particularly high working temperature. Therefore, it is a highly critical element as regards the risk of vulcanization discussed above.
  • the method of the present invention is particularly advantageous since it provides that reaching the working temperature of the nozzle occurs once all the other structural units of the extrusion device have reached their working temperature, thus reducing to the minimum the residence time of the nozzle at such high working temperature before the extrusion process for manufacturing the semi-finished product made of elastomeric material takes place.
  • said at least one drawing member comprises at least one pair of calender rollers.
  • said at least one housing has a working temperature not lower than about 50 °C, more preferably not lower than about 60 °C.
  • said at least one housing has a working temperature not higher than about 120 °C, more preferably not lower than about 90°C.
  • said at least one housing has a working temperature comprised between about 50 °C and about 120 °C, more preferably between about 50 °C and about 90 °C, even more preferably between about 60 °C and 90 °C, even more preferably equal to about 80°C.
  • said at least one member for moving the elastomeric material has a working temperature not lower than about 40°C, more preferably not lower than about 50°C.
  • said at least one member for moving the elastomeric material has a working temperature not higher than about 120 °C, more preferably not higher than about 90°C.
  • said at least one member for moving the elastomeric material has a working temperature comprised between about 40°C and about 120°C, more preferably between about 50 °C and about 90 °C, even more preferably equal to about 80°C.
  • said at least one drawing member has a working temperature not lower than about 70 °C, more preferably not lower than about 90 °C.
  • said at least one drawing member has a working temperature not higher than about 130 °C, more preferably not higher than about 125°C.
  • said at least one drawing member has a working temperature comprised between about 70 °C and about 130 °C, more preferably between about 90°C and about 125°C, even more preferably equal to about 110°C.
  • said at least one gear pump assembly has a working temperature not lower than about 70 °C, more preferably not lower than about 80 °C.
  • said at least one gear pump assembly has a working temperature not higher than about 120 °C, more preferably not higher than about 110°C.
  • said at least one pump assembly has a working temperature comprised between about 70°C and about 120°C, more preferably between about 80°C and about 110°C, even more preferably equal to about 110°C.
  • the working temperatures of said structural units are such as to define a set of increasing temperatures in the following order: member for moving the elastomeric material, housing, drawing member of the elastomeric material.
  • the working temperatures of said structural units are such as to define a set of increasing temperatures in the following order: member for moving the elastomeric material, housing, gear pump assembly and drawing member of the elastomeric material.
  • the thermal inertias of said structural units are such as to define a set of decreasing thermal inertias in the following order: housing, member for moving the elastomeric material, drawing member of the elastomeric material.
  • the thermal inertias of said structural units are such as to define a set of decreasing thermal inertias in the following order: housing, member for moving the elastomeric material, gear pump assembly and drawing member of the elastomeric material.
  • said semi-finished product made of elastomeric material has, in the output section of said drawing member, a thickness not smaller than about 0.5 mm, preferably not smaller than about 0.6 mm.
  • said semi-finished product made of elastomeric material has, in the output section of said drawing member, a thickness not greater than about 4 mm, preferably not greater than about 2 mm.
  • said semi-finished product made of elastomeric material has, in the output section of said drawing member, a thickness comprised between about 0.5 mm and about 4 mm, more preferably between about 0.6 mm and about 2 mm.
  • said semi-finished product made of elastomeric material has, in the output section of said drawing member, a width comprised between about 5 mm and about 25 mm.
  • the elastomeric material is fed into the extrusion device with a flow rate comprised between about 2 cm 3 /s and about 50 cm 3 /s.
  • a flow rate comprised between about 2 cm 3 /s and about 50 cm 3 /s.
  • flow rate values allow limiting the overall cycle time.
  • the heating of the extrusion device is automatically controlled through a remote control unit that also manages the subsequent extrusion of the elastomeric material (when all the structural units of the extrusion device have reached the respective working temperature) for manufacturing the semi-finished product made of elastomeric material .
  • figure 1 is a schematic view of an extrusion device that may be used in the method of the present invention
  • figure 2 shows a diagram that illustrates a heating method of the extrusion device of figure 1 according to the present invention.
  • the present invention has a preferred embodiment thereof in a process for building a component made of elastomeric material of a tyre for vehicle wheels.
  • the above-mentioned process is preferably carried out by providing the movement of a first forming support along a first building line for building a carcass structure comprising at least one carcass ply and a pair of annular anchoring structures, and the movement of a second forming support along a second building line for building a crown structure comprising at least one belt structure and a tread band.
  • the carcass structure and the crown structure thus built are transferred, with a synchronised movement in production-frequency and by respective robot arms, to a workstation for assembling and shaping the tyre being processed, where the carcass structure and the crown structure are reciprocally associated so as to obtain a green tyre.
  • Such green tyre is then transferred on a moulding and curing line for obtaining the finished product .
  • the process for building a component made from elastomeric material of a tyre for vehicle wheels may be carried out in a process for building a tyre wherein the single tyre components are directly built, according to a predetermined frequency, on a single forming support, generally toroidal.
  • the components made of elastomeric material only are obtained starting from a semi-finished product made of elastomeric material only.
  • Such semifinished product is obtained by extrusion and is laid on a forming support while the latter is moved around a rotation axis thereof, so as to obtain a deposition preferably according to adjacent and/or at least partly superimposed coils, according to the component to be made.
  • the extrusion of the semi-finished product takes place at an extrusion device 1 of the type illustrated in figure 1.
  • the semi-finished product obtained through such extrusion device is indicated with 100, whereas the forming support whereon such semi-finished product 100 is laid is indicated with 50.
  • the extrusion device 1 preferably comprises four different structural units, each preferably having mass, thermal inertia (Ii) and working temperature (Ti) different from those of the other structural units.
  • a first structural unit 10 of the extrusion device 10 is defined by a housing 11 in turn defined by a hollow body having a longitudinal axis X-X.
  • the housing 11 comprises, at an upstream end portion 11a thereof, a hopper 12 for loading the elastomeric material to be extruded.
  • a second structural unit 20 of the extrusion device 10 is defined by an extrusion screw 21 rotatably mounted within the housing 11.
  • the extrusion screw 21 acts as a member for moving the elastomeric material within the housing 11.
  • the extrusion screw 21 moves the elastomeric material from the upstream end portion 11a of housing 11 to a downstream end portion lib of housing 11, along a movement direction generally indicated with A.
  • a third structural unit 30 of the extrusion device 10 is preferably defined by a gear pump assembly 31 operatively associated with the housing 11 at the downstream end portion lib thereof.
  • gear pump assembly 31 receives the elastomeric material carried by the extrusion screw 21 and pushes it by pressure downstream, with reference to the moving direction A of the elastomeric material.
  • a fourth structural unit 40 of the extrusion device 10 is preferably defined by a nozzle 41 associated with the gear pump assembly 31 downstream thereof, always with reference to the moving direction A of the elastomeric material, Through such nozzle 41, the elastomeric material pushed by the gear pump assembly 31 is drawn as a semi-finished product 100, to be then laid on the outer surface 50a of the forming support 50.
  • the gear pump assembly 31 pushes the elastomeric material into the nozzle 41 with a pressure not lower than about 30 bar, preferably comprised between about 40 bar and about 600 bar.
  • the elastomeric material is fed towards the forming support 50 with a flow rate preferably not lower than about 2 cm 3 /s, more preferably comprised between about 3 cm 3 /s and about 50 cm 3 /s.
  • Nozzle 41 has an output opening for the elastomeric material shaped so as to define a semi-finished product 100 made of elastomeric material having desired shape and dimensions .
  • the semi-finished product 100 made of elastomeric material is defined by a flat element having, in the output section of said drawing member, a thickness not smaller than about 0.5 mm, preferably not smaller than about 0.6 m, more preferably comprised between about 0.5 mm and about 3 mm, even more preferably comprised between about 0.6 mm and about 2 mm.
  • Said flat element further has, in the output section of said drawing member, a width preferably comprised between about 5 mm and about 25 mm.
  • the working temperatures of said structural units 11, 21, 31, 41 preferably define a set of working temperatures Ti that increase in the following order: extrusion screw 21 (working temperature ⁇ ) , housing 11 (working temperature T 2 ) , gear pump assembly 31 (working temperature T 3 ) and nozzle 41 (working temperature T 4 ) .
  • thermal inertias of said structural units 11, 21, 31, 41 define a set of thermal inertias Ii that decrease in the following order: housing 11 (thermal inertia Ii) , extrusion screw 21 (thermal inertia I 2 ) , gear pump assembly 31 (thermal inertia I 3 ) and nozzle 41 (thermal inertia I 4 ) .
  • the housing 11 has a working temperature (T 2 ) comprised between about 50 °C and about 120 °C, more preferably between about 50°C and about 90°C, even more preferably between about 60 °C and 90 °C, even more preferably equal to about 80°C.
  • T 2 working temperature
  • the extrusion screw 21 has a working temperature (Ti) comprised between about 40 °C and about 120°C, more preferably between about 50°C and about 90°C, even more preferably equal to about 80 °C.
  • Ti working temperature
  • the nozzle 41 has a working temperature (T 4 ) comprised between about 70 °C and about 130 °C, more preferably between about 90 °C and about 125°C, even more preferably equal to about 110°C.
  • T 4 working temperature
  • the gear pump assembly 31 has a working temperature (T3) comprised between about 70°C and about 120°C, more preferably between about 80°C and about 110°C, even more preferably equal to about 100°C.
  • T3 working temperature
  • Each of said structural units 11, 21, 31, 41 is operatively associated with a respective control unit provided for heating the structural unit up to reaching the respective working temperature.
  • the housing 11 is operatively associated with a first control unit 110
  • the extrusion screw 21 is cooperatively associated with a second control unit 120
  • the gear pump assembly 31 is operatively associated with a third control unit 130
  • the nozzle 41 is operatively associated with a fourth control unit 140.
  • Control units 110-140 are all operatively associated with a remote control unit 60 which, besides automatically controlling the heating of said structural units 11, 21, 31, 41, also manages the subsequent extrusion of the elastomeric material once all the structural units 11, 21, 31, 41 have reached the respective working temperature.
  • all the control units 110-140 are set to a first heating temperature T h i having a value equal or close to that of the lowest temperature in the set of temperatures Ti described above, substantially corresponding to the working temperature ⁇ of the extrusion screw 21 (for example, about 60°C).
  • Control units 110-140 are then simultaneously switched on in order to heat all the structural units 11, 21, 31, 41 up to reaching temperature T h i . Since each of said structural units 11, 21, 31, 41 has a mass and a thermal inertia Ii different from that of the other structural units, the heating of the various structural units 11, 21, 31, 41 will take place in different times and according to different heating profiles.
  • the nozzle 41 since the nozzle 41 has a thermal inertia I 4 lower than that of the other structural units, it will be the first to reach temperature T h i (curve a in figure 2), followed in the order by the gear pump assembly 31 (which has a thermal inertia I 3 immediately higher than that of the nozzle 41 - curve b) , the extrusion screw 21 (which has a thermal inertia I 2 immediately higher than that of the pump assembly 31 - curve c) , and the housing 11 (which has a thermal inertia Ii immediately higher than that of the extrusion screw 21 - curve d) .
  • control units 110, 130 and 140 are automatically set to a second temperature value T h2 equal or close to that of the second lower working temperature in the set of temperatures Ti described above, substantially corresponding to the working temperature T 2 of the housing 11 (for example, about 80°C) .
  • control units 130 and 140 are automatically set to a third temperature value T h3 equal or close to that of the third lower working temperature in the set of temperatures Ti described above, substantially corresponding to the working temperature T 3 of the gear pump assembly 31 (for example, about 100°C) .
  • the control unit 140 is automatically set to a fourth temperature value T h4 substantially equal or close to the working temperature T 4 of nozzle 41 (for example about 110°C) .
  • the feeding of the elastomeric material into the hopper 12 of the extrusion device 1 can take place so as to obtain the semi-finished product 100 made of elastomeric material.
  • Such semi-finished product 100 is in turn suitable for being used, in the preferred embodiments of the present invention, for building a component made of elastomeric material of a tyre for vehicle wheels by deposition on the outer surface 50a of said forming support 50.
  • Control units 110, 120, 130 and 140 are suitable for resuming the heating of one or more structural units whose working temperature has already been reached, if one of the working temperatures already reached would drop below a predetermined threshold value before the last working temperature is reached by the corresponding structural unit .
  • the heating temperatures T h i-T h are indicated as equal to the working temperatures ⁇ - ⁇ 4 for simplicity of description only, said temperatures may anyway actually be not exactly matching.
  • the above method may be carried out on extrusion devices consisting of just two structural units too, or on extrusion devices consisting of more than four structural units.
  • the setting and heating operations described above are iteratively repeated multiple times and each time only for the structural units having working temperature Ti higher than the heating temperature T h i set lastly, until all the structural units of the extrusion device have reached the respective working temperature .

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)

Abstract

L'invention porte sur la fabrication d'un produit semi-fini (100) fait d'une matière élastomère. Le procédé selon l'invention est mis en œuvre pour commander la mise à température d'un dispositif d'extrusion (1) qui comprend une pluralité de multiples unités structurales (10-40) qui ont différentes températures de travail (T1-T4) et différentes inerties thermiques (11-14) respectives. Le procédé selon l'invention comprend : a) la définition, pour toutes les unités précitées (10-40), d'une température de chauffage à une valeur égale à, ou proche de, la température de travail de l'unité qui a la plus basse température de travail ; b) le chauffage simultané de toutes les unités précitées (10-40) ; c) lorsque ladite unité s'approche de, ou a atteint, ladite température de chauffage, la définition, pour les autres unités, d'une nouvelle température de chauffage d'une valeur égale à, ou proche de, celle de la température de travail de l'unité dont la température de travail est la plus proche de ladite température de chauffage ; d) répétition itérative des opérations mentionnées sous b) et c) jusqu'à ce que toutes les unités précitées (10-40) aient atteint chacune sa température de travail respective (T1-T4)
PCT/IB2011/001515 2010-06-28 2011-06-27 Procédé pour commander la mise à température d'un dispositif d'extrusion destiné à produire un produit semi-fini en élastomère Ceased WO2012001492A1 (fr)

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JP2013517568A JP5802271B2 (ja) 2010-06-28 2011-06-27 弾性半完成品を製造するための押出成形デバイスの加熱を制御するための方法
EP11743336.7A EP2585272B1 (fr) 2010-06-28 2011-06-27 Procédé pour commander la mise à température d'un dispositif d'extrusion destiné à produire un produit semi-fini en élastomère
CN201180030362.XA CN102958671B (zh) 2010-06-28 2011-06-27 用于控制生产弹性体半成品的挤出装置的加热的方法
KR1020127033188A KR101860449B1 (ko) 2010-06-28 2011-06-27 엘라스토머 반제품 생산을 위해 압출기의 가열을 제어하는 방법
BR112012031733-4A BR112012031733B1 (pt) 2010-06-28 2011-06-27 Método para controlar o aquecimento de um dispositivo de extrusão de um produto semiacabado feito de material elastomérico
US13/807,177 US9403309B2 (en) 2010-06-28 2011-06-27 Method for controlling the heating of an extrusion device of a semi-finished product made of elastomeric material

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ITMI20101171 2010-06-28
ITMI2010A001171 2010-06-28
US36288910P 2010-07-09 2010-07-09
US61/362,889 2010-07-09

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JP2013534481A (ja) 2013-09-05
US9403309B2 (en) 2016-08-02
CN102958671A (zh) 2013-03-06
EP2585272A1 (fr) 2013-05-01
BR112012031733B1 (pt) 2020-02-11
BR112012031733A2 (pt) 2017-05-23
EP2585272B1 (fr) 2017-08-23
US20130106011A1 (en) 2013-05-02

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